Boundary layer devices

ABSTRACT

An aerodynamic or hydrodynamic surface is provided with so-called &#34;riblets&#34; for reducing drag by modification of the turbulent boundary layer. The riblets comprise flow-aligned elongate projections of small height. In order to increase their effectiveness in reducing drag, just those parts of the riblets which extend above the height of the virtual surface--established by the riblets themselves due to their displacing the turbulent motion away from the real surface--exhibit an abrupt transition to a cusp-shaped profile which more effectively promotes very small scale flow-aligned vortices which drain energy from the larger drag-inducing low speed flow-aligned vortices or &#34;streaks&#34; in the boundary layer.

This invention is concerned with the modification of turbulent boundarylayer flows over aerodynamic and hydrodynamic surfaces for the reductionof surface drag. It relates particularly to the provision of so-calledriblet surfaces in which an array of small longitudinal projections orriblets extends over the turbulent boundary layer regions of a wallsurface in the direction of fluid flow over the surface to reduce thesurface drag.

Such riblets may be formed, for example, on plastic tape or sheetmaterial which can be adhered to an underlying surface requiringimproved drag characteristics, such as an aircraft wing, pipeline wallor marine vessel hull, etc., etc. Alternatively, the riblets may beformed directly in the structural skins of such artifacts. Variousmethods of forming the riblets are already known, such as machining,moulding, extruding or embossing In respect of metal riblet,, a furtherpossibility is to form riblets by means of electro-deposition onto amaster, which could be a vinyl plastic

As explained in our earlier patent application Ser. No. 052,867 filedMay 22, 1987, an effect of the riblets of earlier experiments is toinhibit the turbulent eddy motions in the boundary layer frompenetrating to all parts of the surface, in particular deep into thegrooves defined by adjacent riblets, resulting in a displacement of theturbulent motion away from the wall, and thereby a reduction in surfacedrag. Depending upon their profile, the riblet arrays previously knownmay also have had some effect in inhibiting the spanwise gradientsassociated with the formation of the low speed longitudinal vortices or"streaks" that are characteristically formed in a turbulent boundarylayer flow close to a wall, and initiating secondary, smaller-scalelongitudinal eddies which take energy from the larger scale streaks.

It is also possible, as shown in our earlier patent application, todesign an array of projections or riblets so that they not only functionin a mainly passive manner, with little influence on the evolution ofthe eddies themselves, but are also able to exercise some furthercontrol of the longitudinal vortices or streaks, which otherwise shiftin a random manner transversely across the surface, by constraining themlaterally and possible also moving them further apart than their naturalspacing This influence is in substance dependent on those portions ofthe riblets that project into the turbulent motion, i.e. those portionsof the riblets that extend above a virtual wall position that theriblets have themselves created by displacing the turbulent motion awayfrom the wall surface.

According to the present invention, an aerodynamic or hydrodynamic wallsurface adapted to modify a turbulent fluid flow boundary layer on saidsurface has said surface provided with a series of elongate projectionsfor alignment with the direction of fluid flow relative to the surface,at least some of the projections having side faces which intermediatetheir heights have a region at a lesser steepness than adjacent regionsabove and below said region, each said region of lesser steepnessforming the lower part of a concave profile peak on the associatedprojection.

For best effect the transition to the concave-sided peaks should bepositioned at or close to the virtual wall height established by theprojections The height position of the virtual wall will vary accordingto the particular fluid flow regime for which the riblets are designed.The region below the transition preferably has substantially planarfaces so as to form a series of steep-sided V-grooves between theprojections in their lowest reaches These can act in the manner alreadydescribed to displace the turbulent motion away from the wall surface.The longitudinal vortices displaced above the virtual wall surface arethen controlled by the concave peaks projecting into this region which,by virtue of their different profile, can act more strongly on thevortices.

The transition to the concave profile may be substantially sharp-edged,but it is also possible to have a radiussed or chamfered transition. Theconcave faces are preferably continuously curved to a relativelysharp-edged tip but it is also possible to build them up from a group ofstraight and/or curved sections and for convenience the tip itself maybe flattened or radiussed.

In our earlier application, an array of projections is provided on awall surface in which, between each of a series of higher projectionsthere is a plurality of smaller projections. The primary purpose of thesmaller projections is to displace the turbulent motion away from thewall, whereas the higher projections are intended to control the laterallocation of the longitudinal vortices or streaks of the turbulent regionof the boundary layer flow. The displacement produced by the smallerprojections can result in reduced wall shear stress, and to the extentthat the streaks are weakened thereby they can become more amenable tocontrol. Moreover, the disposition of a number of smaller projectionsbetween successive larger projections is able to give a disparity inspanwise scale between the streaks and the smaller projections, as aresult of which the higher projections can promote a more rapid energytransfer from the streaks to the small-scale secondary vortices inducedby these small projections, and they can produce effects that permeateto the region above the smaller projections and so improve theeffectiveness of these projections in that these reduce any activitythere. Through their interaction in these senses the higher and smallerprojections are able to function in an active manner.

The present invention can be applied with advantage to this arrangementof projections so that at least the higher projections have their sidefaces formed with a steepness that varies over their height, with aconcave peak projecting into the turbulent boundary layer motion. To theextent that at least some of the smaller projections extend above thevirtual wall position established by the array, these too preferablyhave their upper regions similarly profiled. If the smaller projectionsare of uniform height, they would then all have such profiled faces.

In our earlier application, a wall surface is provided with an array ofprojections which are disposed in a repeated spanwise pattern in whichthe adjacent projections of each pattern repeat project to differentheights. In the simplest case, this repeated pattern consists ofalternating higher and lower projections. In such a configuration bothsmaller and higher projections can be arranged to displace turbulenteddy motions in the boundary layer away from the wall surface. Whereasthe smaller projections by themselves would not be able to establish avirtual surface above the wall surface by more than about three-quartersof their height, the higher projections can be so scaled in relation tothe smaller projections that they have the function of extending thiseffect to its limit.

When employing the present invention in such configurations as these, atleast the highest projections of the repeat patterns have a variedinclination of the side faces according to the invention. If theenhanced displacement of the virtual wall surface resulting from thecombination of projection heights puts that virtual surface above theheight of the smallest projections, no benefit is achieved by modifyingtheir side faces. To the extent that any of the smaller projectionsextends above the virtual wall position, it is an advantage that theirside faces be given a varied inclination similarly, with the transitionsubstantially at the height of the virtual wall position. This mayresult in a change of inclination occurring at a particular height abovethe actual wall surface that is the origin of the projections, but inparticular cases the pattern or projections may produce a virtual wallsurface height that varies spanwise with the projection pattern, and thepositions of the changes of inclination on the individual projectionscan then follow those changes of height.

Our previous patent application also discloses projections havingprogressively increasing heights with distance along the wall surface inthe direction of fluid wall surface in the direction of fluid flow, soas to counter the self-limiting effect of surface drag reduction as thearray of projections establishes a virtual wall position at asubstantial proportion of the initial height of the projections. In theapplication of the present invention to this configuration, theprojections having a change of steepness intermediate the height oftheir side faces have that change located at a progressively greaterdistance above the actual wall surface with distance along the wallsurface in the direction of fluid flow.

It is to be understood that these modified forms of the configurationsdescribed in our three earlier patent applications can not only be usedindividually but can also be combined, since the effect of themodifications on these different configurations is complementary.

By way of illustration of the invention, reference will be made to theexamples shown in the accompanying schematic drawings, wherein:

FIGS. 1 to 4 illustrate respective configurations, according to theinvention, of projections or riblets in cross-sectional profile normalto the direction of fluid flow, and

FIG. 5 is an illustration of a further projection or ribletconfiguration according to the invention in side view.

FIG. 1 illustrates the application of the present invention to aconfiguration according to our earlier application U.S. serial number052,867. It shows riblets with inclined side faces in a pattern in whichindividual larger riblets R are separated by groups of eight, uniformheight, smaller riblets r. In this it is analogous to the example ofFIG. 1 of that earlier application. In terms of "wall units" as definedin the earlier application, the smaller riblets r have anon-dimensionalised height h⁺ of 15 units above the wall surface and areset at a pitch s⁺ also of 15 units. The larger riblets R have a heighth_(L) ⁺ and width w⁺ of 45 units, so that their pitch s_(L) ⁺ is 165units.

The smaller riblets r establish a virtual surface for the turbulentboundary layer flow some 3/4h⁺ above the wall surface itself and belowthat level all the riblets have planar inclined side faces. At the levelof the virtual surface there is a transition t to a smaller inclinationand the riblets continue upwards from that point of inflection withconcave side faces to a sharp-peaked tip, in analogy to a concave formof riblet also illustrated in our earlier patent application. Above thevirtual wall surface, the larger riblets R have a height (h_(eI) ⁺) of33 wall units, while the corresponding height (h₃ ⁺) of the smallerriblets is about 4 units. The differently profiled regions are adaptedto different functions. The regions below the virtual wall surface formthe relatively deep V-grooves that are better able to inhibitpenetration of turbulent eddy motions, while the concave faces above thevirtual wall surface can more effectively promote very small scalelongitudinal vortices which drain energy from the larger streaks in theturbulent boundary layer flow. To perform their functions effectivelythe V-grooves should have a height:width ratio not substantially greaterthan unity, and the concave faces should form relatively sharp-edgedpeaks.

FIG. 2 illustrates the application of the present invention to a furtherarrangement disclosed in our earlier patent application in which avirtual wall surface is established at the height of the smaller ribletsr in a pattern of alternating riblets of two different heights. Thepattern pitch is 15 wall units, which is therefore the pitch (s⁺, s_(L)⁺) of smaller and larger riblets. The height of the smaller riblets is15 wall units and that of the higher riblets R is 25 wall units; abovethe virtual wall surface they have a height (h_(eI) ⁺) of 13 units forthe larger riblets and (h_(e) ⁺) is about 4 units for the smallerriblets. From the point of transition t the side faces of the ribletsextend upwards with the sharp-peaked concave profiles already describedwhile below the virtual wall surface they form steep-sided V-grooves.

If the presence of the larger riblets has the effect of taking thevirtual wall surface higher the smaller riblets may lie entirely belowthe virtual surface. FIG. 3 illustrates a modification of the example inFIG. 2 in which this occurs and it shows that in addition to the 3/4h⁺displacement of the wall surface produced by the smaller riblets, thelarger riblets induce a further displacement of 3/4h_(eI) ⁺ so that thevirtual wall surface is at a height of (3/4h⁺ +3/4h_(eI) ⁺). The heightof the smaller riblets being less than this their side faces thereforehave a completely planar profile, while side faces of the larger ribletsare given their concave form over their effective height +) from theraised virtual wall surface.

It may be found, however, that a riblet pattern in which the heightchanges between successive riblets produces a similarly undulatingvirtual wall surface, especially if the pattern consists of more thantwo riblets. This can be accommodated by a configuration such as isshown in FIG. 4. Here it is assumed that the virtual wall surface heightfor the smaller riblets r corresponds to that in the example of FIG. 2,whereas for the larger riblets R it corresponds to that in FIG. 3. Thepoint of inflection of the smaller riblets i.e. their intersection withthe virtual surface, is at 3/4h⁺ above the real surface, i.e. the baseline of the pattern of riblets, and for the larger ribs it is at (3/4h⁺+3/4h_(eI) ⁺) above the real surface. The portion of the smaller ribletshaving a concave profile thus extends over a height h_(e) ⁺ =1/4h⁺ whilethe concave profile of the larger riblets extends over a height1/4(h_(L) ⁺ -3/4h⁺)=he⁺ _(II). Similar considerations may apply toconfigurations such as that exemplified in FIG. 1.

Finally FIG. 5 illustrates the application of the present invention to afurther arrangement disclosed in our earlier patent application. In thisthe simple example is taken of a series of riblets which uniformlyincrease in height h⁺ along their lengths, with a virtual wall surfaceat 3/4h⁺. Along the length of the riblets the transition of the upperconcave portions occurs at the same 3/4h⁺ value as h⁺ itself increaseswith distance along the direction of fluid flow.

Similarly to the examples described in our earlier patent application,the change of height of the point of transition can be arrangedstepwise, which may be desirable for ease of production. More generally,the modifications and additional features disclosed for the projectionsin any of the three earlier patent applications referred to can be usedin conjunction with side face configurations according to the presentinvention.

It will be appreciated that the effects described can be achieved, atleast in substance, with modified forms of the inclined side facesshown. In particular, it may be desirable for practical reasons to bluntthe points of inflection or the peaks of the riblet faces, while thesefaces may comprise straight and/or curved portions both below and abovethe virtual wall surface without unduly changing the general characterof the profiles required for the functions described.

Although the above description has focused on achieving improveddrag-reduction per se, a further benefit deriving from the use ofdrag-reducing riblets, achievable by the use of suitable metal, e.g.electro-deposited, riblets on surfaces exposed to fluid-flow, lies inthe field of heat exchange technology. This is because improved heattransfer properties should be associated with reductions in drag. Hence,riblets according to the present invention should maximize the heattransfer efficiency of surfaces to which they are applied

I claim:
 1. An aerodynamic or hydrodynamic wall surface adapted tomodify a turbulent fluid flow boundary layer on said surface, saidsurface being provided with a series of elongate projections foralignment with the direction of fluid flow relative to said surface, atleast some of said projections having side faces which intermediatetheir heights have a region at a lesser steepness than adjacent regionsabove and below said region, each said region of lesser steepnessforming a lower part of a concave profile peak on an associatedprojection,wherein said adjacent region below said region of lessersteepness has a transition to said region of lesser steepness near avirtual wall height position, said virtual wall height position beingdetermined for a predetermined fluid flow regime, by displacement of theboundary layer turbulent flow away from said wall surface by saidprojections; each concave profile peak on an associated projectionhaving a height greater than about three and three quarter wall unitsabove said transition.
 2. A wall surface according to claim 1 whereinsaid series of projections comprise a plurality of higher projectionsbetween successive ones of which there is a plurality of lowerprojections, at least said higher projections having said concaveprofile peaks extending from said regions of lesser steepness.
 3. A wallsurface according to claim 1 wherein said projections are disposed in arepeated spanwise pattern in which adjacent projections of said patternproject to different heights, at least the highest projections havingsaid concave profile peaks extending from said regions of lessersteepness.
 4. A wall surface according to claim 2 or claim 3 whereinthere are both higher and lower projections with said concave profilepeaks extending from said regions of lesser steepness.
 5. A wall surfaceaccording to claim 4 wherein said regions of lesser steepness aredisposed at heights above said wall surface which differ in dependenceupon the heights of said associated projections.
 6. A wall surfaceaccording to claim 4 wherein projections of different heights have saidregions of lesser steepness disposed at a common height.
 7. Anaerodynamic or hydrodynamic wall surface adapted to modify a turbulentfluid flow boundary layer on said surface, said surface being providedwith a series of elongate projections for alignment with the directionof fluid flow relative to said surface, at least some of saidprojections having side faces which intermediate their heights have aregion at a lesser steepness than adjacent regions above and below saidregion, each said region of lesser steepness forming a lower part of aconcave profile peak on an associated projection,wherein said adjacentregion below said region of lesser steepness has a transition to saidregion of lesser steepness near a virtual wall height position, saidvirtual wall height position being determined for a predetermined fluidflow regime, by displacement of the boundary layer turbulent flow awayfrom said wall surface by said projections; said regions of lessersteepness of said projections being located at a height above said wallsurface that increases with distance along said projections in saiddirection of fluid flow.
 8. An aerodynamic or hydrodynamic wall surfaceadapted to modify a turbulent fluid flow boundary layer on said surface,said surface being provided with a series of elongate projections foralignment with the direction of fluid flow relative to said surface, atleast some of said projections having side faces which intermediatetheir heights have a region at a lesser steepness than adjacent regionsabove and below said region, each said region of lesser steepnessforming a lower part of a concave profile peak on an associatedprojection, each said concave profile peak having a height on anassociated projection greater than about three and three quarter wallunits.